Calidus
SYSTEM DESCRIPTION
AutoGyro_POH_Calidus Revision 4.0 – Issue Date 17.JAN.2019 7-26
Other indicators and sensors have been described in the respective paragraphs. For engine
related indicators and sensors see the engine manufacturer’s manual.
7.18 Seats and Seatbelts
The seats consist of seating surface as an integral part of the monocoque structure and
backrest, upholstered with removable cushions. The cushions consist of a foam core
covered with an easily cleanable, water-repellent fabric.
The base cushions are optionally available with a Dynafoam filling. Dynafoam is used to
give increased occupant protection.
The forward backrest hinges are positioned by 4 countersunk Allen bolts on two seating
rails. To suit to different leg lengths the backrest hinges can be adjusted by removing the
Allen bolts and refitting in a different position on the rails.
Hinge attachment screws
Take care to tighten securely, and to ensure both hinges are the same number of holes
from the rearmost position.
In addition the backrest can be adjusted by modifying the lengths of the two adjustment
straps. When adjusting make sure that full travel of the aft control stick is not restricted, if
installed. The aft seat has no adjustment.
An adjustable four point harness is fitted for each seat. Make sure that the aft seat belt is
buckled and tight when flying with the aft seat unoccupied.
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